| 應(yīng)用數(shù)值化材料樣機(jī)對(duì)復(fù)合材料型飛機(jī)葉片進(jìn)行結(jié)構(gòu)分析 |
| 關(guān)鍵詞： |
Elasto-Plastic |
| 類 別： |
復(fù)合材料 >> 其他 |
| 來 源： |
2009 SAMPE |
| 資料類型： |
pdf文件 |
| 資料大?。?/td>
| 537K |
| 簡(jiǎn) 介： |
The objective of this work is to predict the macroscopic elasto-plastic material properties of a jet engine turbine blade loaded by a cyclic centrifugal force. The blade is made of titanium material reinforced by silicon carbide fibers.
DIGIMAT(the nonlinear multi-scale material & structure modeling platform) analyses were first successfully performed to predict the influence of the fibers volume fraction, orientation and aspect ratio on the composite’s elasto-plastic properties.
CADdoctor is used to simplify the geometry and then finite element analyses were performed on the fan blade with ABAQUS |
| 上傳人： |
magicpower |
| 上傳時(shí)間： |
2009-11-10 15:19:20 |
| 下載次數(shù)： |
3 |
| 消耗積分： |
2 |
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